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    Effects of Target Channel Shapes on Double Swirl Cooling Performance at Gas Turbine Blade Leading Edge 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 007:;page 71004
    Author(s): Zhou, Junfei; Wang, Xinjun; Li, Jun; Hou, Weitao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to further study the effects of the target channel shape on the cooling performance of the double swirl cooling (DSC), five double swirl channels formed by two overlapping elliptic cylinders with different length ...
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    Near Tip Loss Control With a Winglet Baffle Cavity Tip in a Turbine Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 010:;page 0101007-1
    Author(s): Li, Li; Jiang, Dengyu; Zhou, Chao; Luo, Hualing; Hou, Weitao; Chang, Qiyue
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamic performance of a winglet baffle cavity tip is investigated at different inlet incidences from −12.5 to +12.5 deg. This blade tip shows a geometry feature with a pressure side winglet and a baffle within the ...
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